EP3365625B1 - Échangeur de chaleur à plaques empilées - Google Patents
Échangeur de chaleur à plaques empilées Download PDFInfo
- Publication number
- EP3365625B1 EP3365625B1 EP16784148.5A EP16784148A EP3365625B1 EP 3365625 B1 EP3365625 B1 EP 3365625B1 EP 16784148 A EP16784148 A EP 16784148A EP 3365625 B1 EP3365625 B1 EP 3365625B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- stacked
- stacking
- heat exchanger
- plate heat
- cavities
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000012530 fluid Substances 0.000 claims description 33
- 239000002826 coolant Substances 0.000 claims description 9
- 230000002093 peripheral effect Effects 0.000 claims description 6
- 238000002485 combustion reaction Methods 0.000 claims description 5
- 239000000498 cooling water Substances 0.000 claims description 3
- 230000002349 favourable effect Effects 0.000 description 8
- 238000007789 sealing Methods 0.000 description 5
- 230000008093 supporting effect Effects 0.000 description 4
- 238000013461 design Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000004891 communication Methods 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004049 embossing Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 230000011218 segmentation Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0031—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other
- F28D9/0043—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other the plates having openings therein for circulation of at least one heat-exchange medium from one conduit to another
- F28D9/005—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other the plates having openings therein for circulation of at least one heat-exchange medium from one conduit to another the plates having openings therein for both heat-exchange media
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B29/00—Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
- F02B29/04—Cooling of air intake supply
- F02B29/045—Constructional details of the heat exchangers, e.g. pipes, plates, ribs, insulation, materials, or manufacturing and assembly
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
- F28F3/08—Elements constructed for building-up into stacks, e.g. capable of being taken apart for cleaning
- F28F3/10—Arrangements for sealing the margins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/008—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for vehicles
- F28D2021/0082—Charged air coolers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0031—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other
- F28D9/0037—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by paired plates touching each other the conduits for the other heat-exchange medium also being formed by paired plates touching each other
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
- F28D9/0062—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for one heat-exchange medium being formed by spaced plates with inserted elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2225/00—Reinforcing means
- F28F2225/04—Reinforcing means for conduits
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2240/00—Spacing means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2280/00—Mounting arrangements; Arrangements for facilitating assembling or disassembling of heat exchanger parts
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the invention relates to a stacked plate heat exchanger, in particular intercooler, with a plurality of stacked stacked disks, wherein in each case a first stacking disk and a second stacking disk are alternately stacked in a stacking direction, wherein the stacking disks each have a set up in a stacking direction and peripheral edge, two adjacent stack disks each abut each other at least with its edge, wherein each two adjacent stack disks define a first cavity for passing a first fluid or a second cavity for passing a second fluid, with first cavities and second cavities alternating in the stacking direction.
- Such stacked plate heat exchangers are used for example in intercoolers. It is passed through the first cavity to be cooled charge air and through the second cavity a coolant. Thus lie on the inner stacking disks on each side of the charge air and on the other side to the cooling medium. As a result, the charge air flowing through the stacked plate heat exchanger can be cooled very effectively by the coolant.
- a stacked plate heat exchanger having a plurality of stacked and interconnected, in particular soldered, elongated discs known that limit a cavity for performing a medium to be cooled in the longitudinal direction of the discs and another cavity for carrying a coolant.
- a stacked plate heat exchanger in which in the cavities a turbulence insert is inserted, which may be formed for example by a corrugated sheet, and which improve the heat transfer from the coolant or the medium to be cooled to the respective stacking disks.
- the present invention has for its object an improved or at least other embodiment of a stacked plate heat exchanger, or a charge air cooler or an internal combustion engine with such a stacked plate heat exchanger to provide, which is characterized in particular by a stabilization of the cavities between the stacking disks.
- the invention is based on the general idea of providing a support device which stabilizes the distance of the individual stacking disks measured in the stacking direction relative to one another. It is expedient for the stacked-plate heat exchanger to have a support device which holds the stacking disks in an edge region of the stack disks is supported against each other in the stacking direction to stabilize the second cavity between the stack disks.
- the support means so the slump of the stacking disks in the stacking direction is additionally limited. Deviations, in particular in the disc length and / or width and / or the angle of the erected edges, thereby have only a very small influence on the self-adjusting distance between the stacking discs. Thereby, the tightness and the stability of the stacked plate heat exchanger can be improved.
- a favorable possibility provides that the support device does not seal the cavity. Because the support device does not have to seal the respective cavity, there are freedoms in the design of the support device that can be used to form a cost-effective and effective support device.
- the support device is different from the edges of the stacking disks. Due to the steep angle of the edges to the stacking disks, small deviations in the angle or in the length or width of the stacking disks lead to a strong displacement of the support point. Consequently, a supporting device based solely on the formation of the edges would not be sufficient to allow a satisfactory support of the spacing of the stacking disks with each other.
- the stacking disks each have, at longitudinal end regions, a first opening for the first fluid and at least two second openings for the second fluid arranged around the first openings.
- the openings formed in the stacking disks thus penetrate in the stacking direction the entire stacking plate heat exchanger. Consequently, through the openings, the respective fluid can flow into the respectively associated cavities.
- fluid flowing through the first openings into the stacked disk heat exchanger may flow only into the first cavities, and fluid flowing through the second openings in the stacked plate heat exchanger may only flow into the second cavities.
- the first cavities formed between the stacking disks and the second cavities are fluidly arranged in each case parallel to one another, that is, through which the respective fluid flows in parallel.
- two fluid passages are formed in the stacked plate heat exchanger, which are separate from each other, so that the coolant and the medium to be cooled do not mix.
- At least a part of the second cavity is formed in a region of the at least one second opening between the stacking disks, and the support device is arranged in the region of the at least one second opening.
- the second openings are located in the edge region of the stacking disks. In this edge region between each two stacking disks alternately a large distance, which forms the second cavity, and no distance, so stacked stacking discs, given. Due to the large distance between the stacking disks in the edge region, the stabilizing effect due to the raised edges is very low. Therefore, the effect of a support device arranged in the region of the at least one second opening is particularly high.
- the stacking disks are shaped in such a way that a stacking disk, in a region of the at least one second opening, has a spacing from a first adjacent stacking disk and rests against another, second adjacent stacking disk lying on the opposite side , In this way, between the two stacking disks in the region of the second openings, either the second cavity is at least partially formed or an effective support of the stacked disks resting on one another is given to one another.
- the supporting device is arranged only in the second cavity between the stacking disks in order to stabilize it.
- a favorable variant provides that the distance of the adjacent stacking disks is defined by the support means.
- the support device can be designed such that a desired defined distance between the stacking disks is set, so that the required height of the respective cavities can be maintained.
- the stacking disks each have at least two second openings for the second fluid arranged around the first openings, webs are formed between the second openings, and at least some of the webs are embossed to form the support means.
- a particularly favorable variant provides that every second web is embossed between the second openings.
- the non-embossed webs can be supported against the lying on the opposite side stacking disks.
- the stacking disks are sufficiently supported in both directions against the adjacent stacking disk.
- the support means is formed by at least one insert part, which is inserted into the second cavity in a region of the at least one second opening.
- the insert part can bridge the distance between the respective stacking disks in the region of the at least one second opening, so that the at least one insert part bears against the two respective stacking disks.
- the respective stacking discs do not approach each other closer, so that is given by the insert sufficient support between the stacking discs.
- the insert is formed substantially semi-annular, wherein on an inner side a plurality of inwardly projecting fingers for segmenting the at least one second opening are arranged.
- a semi-annular insert has the advantage that the position of the insert is stabilized within the second cavity and thus the supporting action of the insert is secured. It is understood that in each end region of the stacking disks at least one insert is inserted in each case. Thus, both end portions of the stacking disks can be stabilized by the support means.
- the support means is formed by a plurality, for example eight, inserts which are inserted into the second cavity in a region of the at least one second openings, and that the inserts are cylindrical.
- Such shaped inserts are extremely cheap to manufacture, so that the support device can be produced inexpensively.
- the support means is formed by at least one cam, which is formed in a variety of stacking disks in the peripheral edge.
- the supporting action of the erected edges is improved, since the stacking disc arranged above the respective stacking disc can not slip over the cams on the edge of the stacking disc.
- the cam blocks further collapse of the stacking disks and thus supports the two stacking disks against each other.
- At least one cam is directed inwards. As a result, the stacking disc following in the stacking direction, which rests against the inside of the raised edge, are blocked by the cam, so that this stacking disc can be supported on the cam.
- a particularly advantageous variant provides that viewed in the stacking direction, the first cavities each lie above one of the first stacking disks, and that the second cavities each lie above one of the second stacking disks. Thereby, the first cavities and the second cavities can be excellently separated from each other fluidly.
- viewed in the stacking direction means that one element, viewed in the stacking direction, over another element is stacked in the direction of the other element. Accordingly, an element that is under another element viewed in the stacking direction, offset from the stacking direction is arranged offset to the other element.
- cams are formed in the edge of the second stacking disks.
- the cams can prevent slippage of the first stacking discs and thus stabilize the second cavities in the region of the second openings of the stacking discs.
- Another particularly favorable solution provides that the first fluid and the second fluid are passed in opposite directions of flow through the stacked plate heat exchanger.
- a heat exchanger is formed in countercurrent principle, which allows a very effective heat exchange between these two media.
- the invention is based on the general idea of providing a charge air cooler with such a stacked plate heat exchanger as described above, wherein charge air of a charging device is the first Fluid is passed through the first cavities and wherein a cooling medium, such as cooling water, is passed as a second fluid through the second cavities.
- a cooling medium such as cooling water
- the invention is based on the general idea of equipping an internal combustion engine with a charging device with a charge air cooler as described above, wherein charge air of the charging device is cooled by the charge air cooler.
- the illustrated unclaimed first embodiment of a stacked plate heat exchanger 10 is used in a charge air cooler for a supercharged internal combustion engine.
- the stacked plate heat exchanger 10 has a plurality of stacked disks 14 stacked on one another in a stacking direction 12.
- the stacked-plate heat exchanger 10 has two types of stacking disks 14, namely first stacking disks 16 and second stacking disks 18.
- the stacking disks 14 have a peripheral edge 20 set up in the stacking direction 12.
- Cavities 22 are formed between the stacking disks 14, wherein first cavities 24 and second cavities 26 alternate in the stacking direction 12.
- the stacking disks 14 have first openings 28 which are arranged in an end region 17 of the stacking disks 14 lying in the longitudinal direction 15 and in second openings 30 which are arranged in the edge regions, for example in a semicircle around the first openings 28.
- a middle region 13 lies between the two end regions 17.
- the stacking disks 14 are in addition to the erected edges 20 embossed to form the cavities 22 between the stacking disks 14.
- the first stacking disk 16 is raised in the stacking direction relative to a base surface 33 in the center region 13 of the first stacking disk 16.
- the region 19 of the at least one second opening 30 is opposite to the stacking direction 12 lowered.
- the stacking disks 14 abut one another in the area 19 of the at least one second opening 30 when a second stacking disk 18 lies above a first stacking disk 16.
- the stack disks 14 form a spacing in the region 19 of the at least one second opening 30 relative to one another when a first stacking disk 16 is arranged above a second stacking disk 18 and thus at least partially form the second cavity 26 there.
- At the areas 19 of the at least one second opening 30 around the at least one second opening 30 around sealing surfaces 29 are formed, which bear against sealing surfaces 29 of the adjacent stacking disks 14.
- the second openings 30 are sealed against the first cavities 24.
- the first openings 28 have a peripheral upstanding edge 31 which is erected from the base surface 33 of the stacking disks 14 in a direction opposite to the direction in which the respective areas 19 of the at least one second opening 30 rise.
- the edges 31 of the first openings 28 are set up in the opposite direction to the stacking direction 12
- the edges 31 of the first openings 28 are set up in the stacking direction 12.
- the height of the edge 31 of the first openings 28 is less than the elevation of the area 19 of the at least one second opening 30.
- the second extend Cavities 26 from the region of the second openings 30 along the entire length of the stacked plate heat exchanger 10 between the second stacking disks 18 and the overlying first stacking disks 16.
- edges 31 of the first openings 28 of two adjacent stacking disks 14 abut each other.
- sealing surfaces 29 are formed on the edges 31. The sealing surfaces 29 seal the first openings 28 against the second cavities 26.
- the second cavities 26 in the region of the second openings 30 have a greater height and taper towards the central region 13.
- the first cavities 24 also taper towards the center region 13 of the stacked plate heat exchanger 10. This is because in the end regions 17, the first cavities 24 and the second cavities 26 are arranged laterally separated from one another, and thus the height between the stacking disks 14 need not be shared.
- the first cavities 24 and the second cavities 26 in the center region 13 of the stacked plate heat exchanger 10 in the stacking direction 12 are separated from each other and extend over the entire surface of the central region 13 of the stacked plate heat exchanger 10. Therefore, the first cavities 24 are tapered and the second cavities 26 respectively from the end portions 17 toward the center hole 13.
- Two fluidically separated fluid passages are formed in the stacked plate heat exchanger 10.
- a first fluid passage is formed through the first cavities 24 and a second fluid passage through the second cavities 26. These fluid passages are in thermal contact with each other via the stacking disks 14, so that a heat exchange between the two fluid passages is given.
- a first fluid for example charge air
- a second fluid for example a coolant
- the flow takes place in the opposite direction, so that a counter-current arrangement is given and thereby the heat between the first fluid and the second fluid can be exchanged particularly effectively.
- the first openings 28 are in fluid communication with the first cavities 24, and the second openings 30 are in fluid communication with the second cavities 26. Via the first openings 28, the first fluid can be passed through the first cavities 24. Via the second openings 30, the second fluid can be passed through the second cavities 26.
- the stacking disks 14 abut one another in the end regions 17 of the stacking disks 14 in the region 19 of the at least one second opening 30, but only if the second stacking disk 18 is arranged above a first stacking disk 16. If a first stacking disk 16 lies above a second stacking disk 18, only an insufficient support between the stacking disks 14 is provided in the end region 17 of the stacking disks 14. As a result, the stacked-plate heat exchanger 10 can be compressed at the end regions 17 in the stacking direction 12, which makes it difficult to assemble the stacked-plate heat exchanger 10. In addition, this can cause leaks.
- a support device 32 is provided, which stabilizes the distance between the stacking disks 14, in particular between second stacking disks 18 and first stacking disks 16, which are each arranged above one of these second stacking disks 18.
- the support device 32 is arranged in an edge region 35 of the stacking disks 14.
- the edge region 35 extends adjacent to the peripheral edge 20 of the stacking disks 14.
- the support device 32 can also support the stacking plates 14 against one another outside the end regions 17 and thus stabilize the cavities 22.
- the support means 32 may be formed by a plurality of inserts 34, which prevents due to their expansion in the stacking direction 12 too strong pushing the stacking disks 14 in the stacking direction 12. As a result, the distance between the stacking disks 14 and thus the second cavities 26 in the region of the second openings is stabilized.
- the inserts 34 are cylindrical. Such cylindrical inserts are very easy to manufacture and thus form a cost-supporting device.
- each pair of stacking disks 14 a plurality of, for example, eight inserts 34 are provided. In each case four inserts are arranged in each of the end regions of the stacked plate heat exchanger 10.
- FIGS. 7 and 8 illustrated unclaimed second embodiment of the stacked plate heat exchanger 10 differs from that in the Fig. 1 to 6 illustrated first embodiment of the stacked plate heat exchanger 10 characterized in that the support means 32 semi-annular Insert 34 is formed with a plurality of inwardly projecting fingers 36.
- the support device 32 per pair of stacking disks 14 two inserts 34, so for each end an insert 34.
- the semi-circular shape of the inserts 34, the position of the inserts 34 within the second cavity 26 are stable, so that the inserts 34, the stacking disks 14th good against each other can support.
- the inwardly projecting fingers 36 of the insertion parts 34 on the one hand cause a segmentation of the second opening 30.
- the position of the inserts 34 within the stacking disks 14 is further defined.
- FIGS. 7 and 8 illustrated second embodiment of the stacked plate heat exchanger 10 with in the Fig. 1 to 6 represented in the first embodiment of the stacked-plate heat exchanger 10 in terms of structure and function, to the above description in this respect reference is made.
- One in the Fig. 9 to 11 illustrated third embodiment of the stacked plate heat exchanger 10 differs from that in the Fig. 1 to 6 shown in that the stacking disks 14 have a plurality of second openings 30 which are separated by webs 38 and in that the support means 32 is formed by embossed webs 39 between the second openings 30.
- the stacking disks 14 have a plurality of second openings 30 which are separated by webs 38 and in that the support means 32 is formed by embossed webs 39 between the second openings 30.
- embossed webs 39 and non-embossed webs 37 are arranged.
- the embossed webs 39 are embossed in such a way that they protrude into the later-formed second cavity 26.
- the embossed webs 39 of the first stacking disk 16 and the second stacking disk 18 can mutually support one another.
- the stacking disks 14 can in both directions in the region 19 of the at least one second opening 30 are supported against the adjacent stacking disks 14.
- FIGS. 12 and 13 illustrated unclaimed fourth embodiment of the stacked plate heat exchanger 10 differs from that in the Fig. 9 to 11 illustrated third embodiment of the stacked plate heat exchanger 10 characterized in that the support means 32 is formed by a plurality, for example five, introduced into the edge 20 of the second stacking disks 18 cam 40.
- the cams 40 are preferably directed inwards.
- the first stacking disks 16, which are arranged above the second stacking disks 18, can thus be supported by the cams 40.
- the distance between the stacking disks 14 in the region of the second opening 30 is stabilized by the cams 40.
- FIGS. 12 and 13 illustrated unclaimed fourth embodiment of the stacked plate heat exchanger 10 with in the Fig. 9 to 11 illustrated third embodiment of the stacked-plate heat exchanger 10 with respect to structure and function match, the above description of which reference is made.
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Claims (5)
- Échangeur de chaleur à plaques empilées, en particulier pour un refroidisseur d'air de suralimentation, avec plusieurs plaques empilées (14, 16, 18) empilées les unes sur les autres,- dans lequel respectivement une première plaque empilée (14, 16) et une seconde plaque empilée (14, 18) sont empilées en alternance l'une sur l'autre dans un sens d'empilement (12),- dans lequel les plaques empilées (14, 16, 18) présentent respectivement un bord (20) tournant et placé dans un sens d'empilement (12),- dans lequel deux plaques empilées (14, 16, 18) contigües reposent respectivement au moins avec leur bord (20) l'une contre l'autre,- dans lequel respectivement deux plaques empilées (14, 16, 18) contigües délimitent une première cavité (22, 24) pour la réalisation d'un premier fluide ou une seconde cavité (22, 26) pour la réalisation d'un second fluide, dans lequel des premières cavités (24) et des secondes cavités (26) alternent dans le sens d'empilement (12),- dans lequel l'échangeur de chaleur à plaques empilées (10) présente un dispositif d'appui (32) qui appuie les unes contre les autres les plaques empilées (14, 16, 18) dans une zone d'appui (35) des plaques empilées (14, 16, 18) afin de stabiliser la seconde cavité (22, 26) entre les plaques empilées (14, 16, 18),- dans lequel les plaques empilées (14, 16, 18) présentent au niveau de zones d'extrémité (17) se trouvant dans le sens longitudinal (15) respectivement une première ouverture (28) pour le premier fluide et respectivement au moins deux secondes ouvertures (30) agencées autour des premières ouvertures (28) pour le second fluide,- dans lequel dans une zone (19) des au moins deux secondes ouvertures (30) entre les plaques empilées (14, 16, 18) au moins une partie de la seconde cavité (22, 26) est formée,- dans lequel le dispositif d'appui (32) est agencé dans la zone (19) des au moins deux secondes ouvertures (30),- dans lequel des traverses (38) sont formées entre les secondes ouvertures (30), et caractérisé en ce- qu'au moins certaines des traverses (38) sont gaufrées de sorte que les traverses gaufrées (38) pénètrent dans la seconde cavité (22, 26) et reposent contre une traverse gaufrée (38) des plaques empilées (14, 16, 18) contigües afin de former le dispositif d'appui (32).
- Échangeur de chaleur à plaques empilées selon la revendication 1,
caractérisé en ce
que les plaques empilées (14, 16, 18) sont formées de telle manière qu'une plaque empilée (14, 16, 18) présente une distance dans une zone (19) d'au moins une seconde ouverture (30) à un première plaque empilée (14, 16, 18) contigüe et repose contre une autre seconde plaque empilée (14, 16, 18) contigüe se trouvant sur le côté opposé. - Échangeur de chaleur à plaques empilées selon la revendication 2,
caractérisé en ce
que la distance des plaques empilées (14, 16, 18) contigües est définie par le dispositif d'appui (32). - Refroidisseur d'air de suralimentation avec un échangeur de chaleur à plaques empilées (10) selon l'une des revendications 1 à 3,
caractérisé en ce- que de l'air de suralimentation d'un dispositif de suralimentation est acheminé comme premier fluide par les premières cavités (24),- qu'un fluide de refroidissement, par exemple de l'eau de refroidissement, est acheminé comme second fluide par les secondes cavités (26). - Moteur à combustion interne avec un dispositif de suralimentation et un refroidisseur d'air de suralimentation selon la revendication 4, dans lequel de l'air de suralimentation du dispositif de suralimentation est refroidi par le refroidisseur d'air de suralimentation.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102015220579.7A DE102015220579A1 (de) | 2015-10-21 | 2015-10-21 | Stapelscheiben-Wärmeübertrager |
| PCT/EP2016/074337 WO2017067820A2 (fr) | 2015-10-21 | 2016-10-11 | Échangeur de chaleur à plaques empilées |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP3365625A2 EP3365625A2 (fr) | 2018-08-29 |
| EP3365625B1 true EP3365625B1 (fr) | 2019-12-04 |
Family
ID=57153451
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP16784148.5A Active EP3365625B1 (fr) | 2015-10-21 | 2016-10-11 | Échangeur de chaleur à plaques empilées |
Country Status (6)
| Country | Link |
|---|---|
| US (2) | US10852067B2 (fr) |
| EP (1) | EP3365625B1 (fr) |
| KR (1) | KR101933946B1 (fr) |
| CN (1) | CN208688305U (fr) |
| DE (1) | DE102015220579A1 (fr) |
| WO (1) | WO2017067820A2 (fr) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SE544093C2 (en) * | 2019-05-21 | 2021-12-21 | Alfa Laval Corp Ab | Plate heat exchanger, and a method of manufacturing a plate heat exchanger |
| DK180418B1 (en) * | 2019-11-07 | 2021-04-22 | Danfoss As | Heat exchanger plate |
| DE102020201131A1 (de) * | 2020-01-30 | 2021-08-05 | Mahle International Gmbh | Wärmeübertrager-Platte für einen Wärmeübertrager, insbesondere für einen Stapelscheiben-Wärmeübertrager oder für einen Platten-Wärmeübertrager |
| JP7194764B2 (ja) * | 2021-02-08 | 2022-12-22 | 株式会社日阪製作所 | プレート式熱交換器 |
| FR3130021B1 (fr) * | 2021-12-08 | 2023-10-27 | Valeo Systemes Thermiques | Échangeur thermique pour véhicule automobile |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6113178U (ja) * | 1984-06-28 | 1986-01-25 | 株式会社 土屋製作所 | ハウジングレス熱交換器 |
| EP0183398B1 (fr) | 1984-11-30 | 1989-04-12 | FISONS plc | Inhibiteurs d'enzyme transformant l'angiotensine, leur préparation et leur application comme produits pharmaceutiques |
| US4872578A (en) * | 1988-06-20 | 1989-10-10 | Itt Standard Of Itt Corporation | Plate type heat exchanger |
| SE462763B (sv) * | 1989-04-28 | 1990-08-27 | Torell Ab | Plattvaermevaexlare/kylare samt saett att tillverka denna |
| US5435383A (en) * | 1994-02-01 | 1995-07-25 | Rajagopal; Ramesh | Plate heat exchanger assembly |
| DE19511991C2 (de) | 1995-03-31 | 2002-06-13 | Behr Gmbh & Co | Plattenwärmetauscher |
| DE59600935D1 (de) | 1995-05-10 | 1999-01-21 | Laengerer & Reich Gmbh & Co | Plattenwärmetauscher |
| DE19605340C2 (de) * | 1996-02-14 | 2000-11-09 | Behr Gmbh & Co | Wärmeübertrager und Verfahren zu seiner Herstellung |
| DE29616354U1 (de) | 1996-09-19 | 1997-01-09 | Laengerer & Reich Gmbh & Co | Abgaswärmetauscher |
| JP2002518659A (ja) * | 1998-06-12 | 2002-06-25 | チャート、ヒート、エクスチェンジャーズ、リミテッド | 熱交換器 |
| EP1083398A1 (fr) | 1999-09-10 | 2001-03-14 | Toyo Radiator Co., Ltd. | Echangeur de chaleur à plaques et son procédé de fabrication |
| DE102005044291A1 (de) | 2005-09-16 | 2007-03-29 | Behr Industry Gmbh & Co. Kg | Stapelscheiben-Wärmeübertrager, insbesondere Ladeluftkühler |
| DE102006044154A1 (de) * | 2006-09-15 | 2008-05-21 | Behr Gmbh & Co. Kg | Stapelscheibenwärmetauscher zur Ladeluftkühlung |
| US8678076B2 (en) | 2007-11-16 | 2014-03-25 | Christopher R. Shore | Heat exchanger with manifold strengthening protrusion |
| DE102010028660A1 (de) * | 2010-05-06 | 2011-11-10 | Behr Industry Gmbh & Co. Kg | Stapelscheiben-Wärmetauscher |
| DE102010036664B4 (de) * | 2010-07-27 | 2017-07-20 | Peter Rehberg | Plattenwärmeübertrager |
| US9417016B2 (en) * | 2011-01-05 | 2016-08-16 | Hs Marston Aerospace Ltd. | Laminated heat exchanger |
-
2015
- 2015-10-21 DE DE102015220579.7A patent/DE102015220579A1/de not_active Withdrawn
-
2016
- 2016-10-11 KR KR1020187011257A patent/KR101933946B1/ko not_active Expired - Fee Related
- 2016-10-11 US US15/770,189 patent/US10852067B2/en not_active Expired - Fee Related
- 2016-10-11 WO PCT/EP2016/074337 patent/WO2017067820A2/fr not_active Ceased
- 2016-10-11 EP EP16784148.5A patent/EP3365625B1/fr active Active
- 2016-10-11 CN CN201690001282.XU patent/CN208688305U/zh not_active Expired - Fee Related
-
2020
- 2020-07-08 US US16/924,168 patent/US11680751B2/en active Active
Non-Patent Citations (1)
| Title |
|---|
| None * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN208688305U (zh) | 2019-04-02 |
| KR20180054806A (ko) | 2018-05-24 |
| DE102015220579A1 (de) | 2017-04-27 |
| WO2017067820A2 (fr) | 2017-04-27 |
| KR101933946B1 (ko) | 2018-12-31 |
| US20200340750A1 (en) | 2020-10-29 |
| EP3365625A2 (fr) | 2018-08-29 |
| WO2017067820A3 (fr) | 2017-06-15 |
| US20180328672A1 (en) | 2018-11-15 |
| US11680751B2 (en) | 2023-06-20 |
| US10852067B2 (en) | 2020-12-01 |
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